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LEMUR 2 MJR092620

In orbit NORAD 58340 PCCO-9403-6164-4867-7658 United States of America

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
LEMUR 2 MJR092620
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2023-11-11 00:00:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
413.08 km
Apogee
421.43 km
Inclination
97.4°
Period
93.0 min
Semi-major axis
6795.4 km
Velocity
7.64 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 20:56:57 UTC
Two-line elements (TLE)
1 58340U 23174CN  26283.50188481  .00022091  00000-0  41248-3 0  9999
2 58340 97.3953 15.9633 0006145 66.4483 293.7412 15.48767885163470
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-13 06:55:47 STARLINK-1153
NORAD 45080
LEMUR-2-MJR092620
NORAD 58340
1.034 9.39 1.0e-04
2026-10-15 23:37:15 STARLINK-1422
NORAD 45696
LEMUR-2-MJR092620
NORAD 58340
1.468 9.89 4.9e-05
2026-10-16 01:56:45 STARLINK-1422
NORAD 45696
LEMUR-2-MJR092620
NORAD 58340
3.231 9.87 1.0e-05
2026-10-16 13:19:11 LEMUR-2-MJR092620
NORAD 58340
OBJECT AS
NORAD 61775
1.652 14.26 7.7e-07
2026-10-16 19:03:57 LEMUR-2-MJR092620
NORAD 58340
ELECTRON KICK STAGE R/B
NORAD 100748
2.323 12.97 4.9e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite